Neural inverse-based fast control of quadrotors with actuator saturation.

Yiming Wang, Hao An, Linchang Lu
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引用次数: 0

Abstract

This study investigates the fast attitude control for quadrotors subject to possible actuator saturations. A low-complexity neural dynamic inverse is constructed to decouple attitude dynamics without applying the conventional small-angle assumption. Aiming at decoupled dynamics with mismatched disturbances, an improved terminal sliding mode controller is designed to realize the fast attitude regulation. In particular, a novel anti-windup mechanism and a finite-time disturbance observer are constructed, respectively, to evaluate motor saturations and estimate mismatched disturbances online, whose information is employed to optimize the baseline terminal sliding mode controller. The effectiveness of the proposed control has been theoretically proven and practically tested.

基于神经逆的驱动器饱和四旋翼快速控制。
本文研究了受致动器可能饱和影响的四旋翼飞行器的快速姿态控制。构造了一种低复杂度的神经动力学逆来解耦姿态动力学,而不采用传统的小角度假设。针对存在不匹配扰动的解耦动力学问题,设计了一种改进型末端滑模控制器,实现了姿态的快速调节。特别地,构建了一种新的抗卷绕机构和有限时间干扰观测器,分别用于在线评估电机饱和和估计不匹配干扰,并利用其信息优化基线终端滑模控制器。所提出的控制方法的有效性已得到理论证明和实践检验。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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